ACwing FC firmware
STM32WB55: attitude IEKF, altitude Kalman filter, flight core, protocol v2
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ctrl_att_in_t Struct Reference

#include <control_hooks.h>

Data Fields

float q [4]
 IEKF attitude, body->world NWU, [w x y z].
 
float dt
 
uint32_t step
 

Detailed Description

Definition at line 25 of file control_hooks.h.

Field Documentation

◆ q

float ctrl_att_in_t::q[4]

IEKF attitude, body->world NWU, [w x y z].

Definition at line 26 of file control_hooks.h.

Referenced by on_acc_window().

◆ dt

float ctrl_att_in_t::dt

Definition at line 27 of file control_hooks.h.

Referenced by on_acc_window().

◆ step

uint32_t ctrl_att_in_t::step

Definition at line 28 of file control_hooks.h.

Referenced by on_acc_window().


The documentation for this struct was generated from the following file: